整体复合材料油箱壁板原位无损检测技术  

In-situ Nondestructive Testing Technology for the Integral Composite Panel of the Fuel Tank

作　　者：王丹[1] 宁宁[1] 杨鹏飞[1] 詹绍正[1] 黄华斌[1] WANG Dan;NING Ning;YANG Pengfei;ZHAN Shaozheng;HUANG Huabin(Aircraft Strength Research Institute,Xi＇an 710065,China)

机构地区：[1]中国飞机强度研究所,西安710065

出　　处：《无损检测》2018年第11期33-36,55,共5页Nondestructive Testing

摘　　要：针对复合材料机翼油箱原位检测效率、油箱残留油液影响超声检测结果评判等问题,结合某机型复合材料机翼油箱壁板的结构形式、损伤特征及实际外场检测环境等特点,开展了机翼油箱整体壁板超声相控阵快速化原位检测和油液对超声检测信号的影响研究。最终建立了飞机复合材料机翼油箱整体壁板的超声相控阵快速化检测方案和含油液条件下超声检测脱黏损伤的评定方法。This paper aims at the problems of the in situ detection efficiency of the composite wing tank and the influence of residual oil in oil tank on ultrasonic evaluation.By the overall consideration of the composite wing tank structure form of the aircraft,the damage characteristics and actual field detection environment,researches on the rapid in-situ detection of the whole wall panel of the wing tank by ultrasonic phased array and on the influence of aircraft oil on ultrasonic testing signals are carried out.Finally,the rapid detection scheme of ultrasonic phased array for the integral panel of the aircraft composite wing fuel tank and the design of the evaluation method of debonding damage by ultrasonic testing under the existence of aircraft oil were proposed.

关 键 词：复合材料机翼油箱 原位检测 超声相控阵 飞机燃油 脱黏 

分 类 号：TG115.28[金属学及工艺—物理冶金] V258[金属学及工艺—金属学]